File Download

There are no files associated with this item.

  • Find it @ UNIST can give you direct access to the published full text of this article. (UNISTARs only)
Related Researcher

손흥선

Son, Hungsun
Electromechanical System and control Lab.
Read More

Views & Downloads

Detailed Information

Cited time in webofscience Cited time in scopus
Metadata Downloads

Full metadata record

DC Field Value Language
dc.citation.startPage 105549 -
dc.citation.title AEROSPACE SCIENCE AND TECHNOLOGY -
dc.citation.volume 96 -
dc.contributor.author Xia, Kewei -
dc.contributor.author Lee, Sangheon -
dc.contributor.author Son, Hungsun -
dc.date.accessioned 2023-12-21T18:10:44Z -
dc.date.available 2023-12-21T18:10:44Z -
dc.date.created 2019-12-12 -
dc.date.issued 2020-01 -
dc.description.abstract The autonomous ship landing control issue of multi-rotor Unmanned Aerial Vehicles (UAVs) is investigated. To achieve the ship landing operation efficiently and precisely, a novel mission planning consisting of an approaching stage and a landing stage is first proposed, where the desired altitude for the UAV is provided according to the requirements in each stage. Affected by rough sea wave, a feasible final landing condition is planned such that the UAV could land on the ship board in a safe environment. Then, the solution to the ship landing operation is transformed into the UAV trajectory tracking. Due to the under-actuated nature of the UAV, an adaptive robust hierarchical algorithm is developed such that the position tracking to the desired trajectory and the attitude tracking to the command attitude are achieved. In particular, an asymmetric saturated command force is designed by introducing a dynamic compensator to ensure the nonsingular attitude extraction, and a tracking error constrained applied torque is exploited to avoid the nature singularity of Euler angle in sequence. The asymptotic stability of the closed-loop system is analyzed in view of the hierarchical system stability theory. Simulations are performed to validate the proposed strategy. -
dc.identifier.bibliographicCitation AEROSPACE SCIENCE AND TECHNOLOGY, v.96, pp.105549 -
dc.identifier.doi 10.1016/j.ast.2019.105549 -
dc.identifier.issn 1270-9638 -
dc.identifier.scopusid 2-s2.0-85076042269 -
dc.identifier.uri https://scholarworks.unist.ac.kr/handle/201301/30591 -
dc.identifier.url https://www.sciencedirect.com/science/article/pii/S1270963819312477 -
dc.identifier.wosid 000510081700045 -
dc.language 영어 -
dc.publisher Elsevier BV -
dc.title Adaptive control for multi-rotor UAVs autonomous ship landing with mission planning -
dc.type Article -
dc.description.isOpenAccess FALSE -
dc.relation.journalWebOfScienceCategory Engineering, Aerospace -
dc.relation.journalResearchArea Engineering -
dc.type.docType Article -
dc.description.journalRegisteredClass scie -
dc.description.journalRegisteredClass scopus -
dc.subject.keywordAuthor Ship landing of multi-rotor UAV -
dc.subject.keywordAuthor Mission planning -
dc.subject.keywordAuthor Adaptive control -
dc.subject.keywordAuthor Non-singularity -
dc.subject.keywordPlus TRAJECTORY TRACKING CONTROL -
dc.subject.keywordPlus SLIDING MODE CONTROL -
dc.subject.keywordPlus UNMANNED AERIAL VEHICLE -
dc.subject.keywordPlus QUADROTOR UAV -
dc.subject.keywordPlus CONTROL DESIGN -
dc.subject.keywordPlus HELICOPTER -
dc.subject.keywordPlus COMPENSATION -
dc.subject.keywordPlus SATURATION -
dc.subject.keywordPlus VESSEL -

qrcode

Items in Repository are protected by copyright, with all rights reserved, unless otherwise indicated.